FR3052522B1 - Dispositif de recuperation d'huile de lubrification ejectee par effet centrifuge dans une turbomachine - Google Patents

Dispositif de recuperation d'huile de lubrification ejectee par effet centrifuge dans une turbomachine Download PDF

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Publication number
FR3052522B1
FR3052522B1 FR1655332A FR1655332A FR3052522B1 FR 3052522 B1 FR3052522 B1 FR 3052522B1 FR 1655332 A FR1655332 A FR 1655332A FR 1655332 A FR1655332 A FR 1655332A FR 3052522 B1 FR3052522 B1 FR 3052522B1
Authority
FR
France
Prior art keywords
turbomachine
lubricating oil
centrifugal effect
oil ejected
recovering lubricating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1655332A
Other languages
English (en)
Other versions
FR3052522A1 (fr
Inventor
Phorla Lao Jeremy
Olivier BELMONTE
Charlotte Marie Mouton Clementine
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1655332A priority Critical patent/FR3052522B1/fr
Priority to GB1709060.6A priority patent/GB2552883B/en
Priority to US15/618,915 priority patent/US10280795B2/en
Publication of FR3052522A1 publication Critical patent/FR3052522A1/fr
Application granted granted Critical
Publication of FR3052522B1 publication Critical patent/FR3052522B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/06—Arrangements of bearings; Lubricating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/042—Guidance of lubricant
    • F16H57/0421—Guidance of lubricant on or within the casing, e.g. shields or baffles for collecting lubricant, tubes, pipes, grooves, channels or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/042—Guidance of lubricant
    • F16H57/0421—Guidance of lubricant on or within the casing, e.g. shields or baffles for collecting lubricant, tubes, pipes, grooves, channels or the like
    • F16H57/0424—Lubricant guiding means in the wall of or integrated with the casing, e.g. grooves, channels, holes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/042—Guidance of lubricant
    • F16H57/0427—Guidance of lubricant on rotary parts, e.g. using baffles for collecting lubricant by centrifugal force
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/0467—Elements of gearings to be lubricated, cooled or heated
    • F16H57/0479—Gears or bearings on planet carriers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/048—Type of gearings to be lubricated, cooled or heated
    • F16H57/0482—Gearings with gears having orbital motion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/609—Deoiling or demisting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/98—Lubrication
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Details Of Gearings (AREA)
FR1655332A 2016-06-10 2016-06-10 Dispositif de recuperation d'huile de lubrification ejectee par effet centrifuge dans une turbomachine Active FR3052522B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1655332A FR3052522B1 (fr) 2016-06-10 2016-06-10 Dispositif de recuperation d'huile de lubrification ejectee par effet centrifuge dans une turbomachine
GB1709060.6A GB2552883B (en) 2016-06-10 2017-06-07 Device for recovering lubrication oil ejected by centrifugal effect in a turbine engine
US15/618,915 US10280795B2 (en) 2016-06-10 2017-06-09 Device for recovering lubrication oil ejected by centrifugal effect in a turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1655332A FR3052522B1 (fr) 2016-06-10 2016-06-10 Dispositif de recuperation d'huile de lubrification ejectee par effet centrifuge dans une turbomachine
FR1655332 2016-06-10

Publications (2)

Publication Number Publication Date
FR3052522A1 FR3052522A1 (fr) 2017-12-15
FR3052522B1 true FR3052522B1 (fr) 2018-06-01

Family

ID=56611425

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1655332A Active FR3052522B1 (fr) 2016-06-10 2016-06-10 Dispositif de recuperation d'huile de lubrification ejectee par effet centrifuge dans une turbomachine

Country Status (3)

Country Link
US (1) US10280795B2 (fr)
FR (1) FR3052522B1 (fr)
GB (1) GB2552883B (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3473893B1 (fr) * 2017-10-19 2020-06-17 Ge Avio S.r.l. Collecte de fluide de lubrification dans une boîte de vitesses d'un moteur à turbine à gaz
FR3081513B1 (fr) * 2018-05-28 2021-06-18 Safran Aircraft Engines Systeme de transmission de puissance comprenant un dispositif de recuperation d'huile de lubrification et turbomachine equipee d'un tel systeme de transmission de puissance
FR3084407B1 (fr) * 2018-07-26 2021-04-30 Safran Aircraft Engines Gouttiere de canalisation d'huile de lubrification d'une turbomachine d'aeronef
US11401833B2 (en) 2018-12-10 2022-08-02 Raytheon Technologies Corporation Seal oil systems
US10989073B2 (en) * 2019-03-05 2021-04-27 Rolls-Royce Corporation Power gearbox with embedded oil reservoir for use in a gas turbine engine
FR3095243B1 (fr) * 2019-04-19 2021-04-30 Safran Aircraft Engines Reducteur de vitesse d’une turbomachine
FR3097011B1 (fr) * 2019-06-06 2022-02-18 Safran Aircraft Engines Reducteur planetaire pour une turbomachine d’aeronef
FR3103240B1 (fr) * 2019-11-15 2022-07-15 Safran Aircraft Engines Rouet pour un porte-satellites de reducteur de vitesse a train epicycloïdal de turbomachine
FR3104193B1 (fr) * 2019-12-10 2021-10-29 Safran Aircraft Engines Recuperation d’huile de lubrification d’un reducteur de turbomachine d’aeronef
CN111878237B (zh) * 2020-07-29 2021-11-16 中国航发湖南动力机械研究所 收油环及环下供油润滑装置
FR3117171B1 (fr) 2020-12-03 2022-10-21 Safran Systeme de transmission de puissance comportant une gouttiere de recuperation d’huile amelioree

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB369875A (en) * 1930-11-17 1932-03-31 Avions H M D Farman Improvements in and relating to the lubrication of internal combustion engines
DE3819519A1 (de) * 1988-06-08 1989-12-21 Siemens Ag Vorrichtung zur sicherung der anlaufschmierung eines in einem getriebekasten angeordneten untersetzungsgetriebes
US6223616B1 (en) * 1999-12-22 2001-05-01 United Technologies Corporation Star gear system with lubrication circuit and lubrication method therefor
EP2834503B1 (fr) 2012-02-23 2018-04-11 Safran Aircraft Engines Dispositif de récupération de l'huile de lubrification d'un réducteur épicycloïdal
FR2987402B1 (fr) * 2012-02-23 2015-02-27 Snecma Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire.

Also Published As

Publication number Publication date
GB2552883B (en) 2022-02-23
FR3052522A1 (fr) 2017-12-15
GB201709060D0 (en) 2017-07-19
US10280795B2 (en) 2019-05-07
US20170356306A1 (en) 2017-12-14
GB2552883A (en) 2018-02-14

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